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Austrian Space Law Newsletter
Austrian Space Law Newsletter Number 16 , June 2017 Editorial 2 Interview with Simonetta Di Pippo 3 The International Astronautical Congress (IAC) 6 Interview with Andreas Geisler 8 ”Big Data” at the Global Conference on Space and the Information Society (GLIS) 11 GLIS 11 Interview with David Kendall 13 NPOC Symposium ”Looking to the Future: Changing International Relations and Legal Issues Facing Space Activities” 17 Interview with Jean-Jacques Tortora 18 “Born to Explore”: the 29th Planetary Congress of the Association of Space Explorers 20 Interview with Franz Viehböck 23 Space Law at the Vienna Humanities Festival 26 “Born to Explore” 20 Women in Aerospace Europe: Vienna Local Group Launch Event 27 Manfred Lachs Space Law Moot Court Competition 2016 28 25th ECSL Summer Course on Space Law and Policy 2016 29 NPOC Space Law Austria Subpoint Graz Outreach Activities 2016 30 Seminar on Space Law and Space Policy at the University of Graz 2016 30 Humanities Festival 26 Upcoming Events 31 EDITORIAL Irmgard Marboe The year 2017 marks the 50th Viehböck, the first and only Austrian astronaut, at the margins anniversary of the legal foun- of the 29th Planetary Congress of the Association of Space dation of international space Explorers which took place in Austria in autumn 2016, shares law, the Outer Space Treaty. experiences and perspectives 25 years after the Austromir Opened for signature on 27 mission with Cordula Steinkogler who did not only conduct January 1967, it entered into all the interviews but was also in the ÖWF (Österreichisches force on 10 October in the Weltraum Forum) organising team of the Planetary Congress. -
Polski Sektor Kosmiczny EN.Indd
Cassini-Huygens Mars Express POLAND IN ESA BRITE-PL „Lem” Meteor 2 Kopernik 500 Integral Rosetta Mikołaj Kopernik REACHING STARS Jan Heweliusz Mirosław — Hermaszewski POLISH SPACE SECTOR 4 years in ESA PW-SAT BRITE-PL „Heweliusz” Herschel Vertical-1 ExoMars TABLE OF CONTENTS Poland 3 History of space activities 4 Space policy 6 In space and on Earth 8 Companies 12 Selected scientific and research institutions 19 Competence map 22 2 WTO UN 01 OECD POLAnd Population: 38.4 million NATO Area: 312 000 km2 Economy: 23rd place in the world* Capital city: Warsaw Government system: parliamentary republic Currency: złoty (PLN) EU ESA * World Bank, 2015, GDP based on PPP EDA EUMETSAT ESO POLAND POLAND CENTRAL AND EasterN EUROPE EU28 GDP (PPP) per capita of Poland compared Economic growth in Poland and EU28 to other countries of Central and Eastern Europe Source: own compilation based on data from Eurostat Source: The Global Competitiveness Report, World Economic Forum 3 02 HISTORY OF SPACE ACTIVITIES The beginning of Polish engagement in space flights presence of Polish instruments on the majority of the stemmed from participation in the international pro- Agency’s research missions. Meanwhile, the first private gramme Interkosmos, based on collaboration with the Polish companies offering satelite-based applications Soviet Union. The first Polish research device was sent and services were created. into orbit on board the satellite Kopernik-500 (Interkos- In 2007, the signing of the Plan for European Coope- mos-9) in 1973. Three years later the Space Research rating States (PECS) enabled significant extension of Centre of the Polish Academy of Sciences was estab- Poland’s cooperation with ESA. -
The BRITE-Constellation Nanosatellite Space Mission and Its First Scientific Results
EPJ Web of Conferences 160, 01001 (2017) DOI: 10.1051/epjconf/201716001001 Seismology of the Sun and the Distant Stars II The BRITE-Constellation Nanosatellite Space Mission And Its First Scientific Results G. Handler1,, A. Pigulski2, W. W. Weiss3, A.F.J.Moffat4, R. Kuschnig3,5, G. A. Wade6, P. Orleanski´ 7, S. M. Rucinski´ 8, O. Koudelka5, R. Smolec1, K. Zwintz9, J. M. Matthews10, A. Popowicz11, D. Baade12, C. Neiner13, A. A. Pamyatnykh1, J. Rowe14, and A. Schwarzenberg-Czerny1 1Nicolaus Copernicus Astronomical Center, Bartycka 18, 00-716 Warsaw, Poland 2Instytut Astronomiczny, Uniwersytet Wrocławski, ul. Kopernika 11, 51-622 Wrocław, Poland 3Institute for Astrophysics, Universität Wien, Türkenschanzstrasse 17, A-1180 Wien, Austria 4Départment de physique, Université de Montréal, C. P. 6128, Succ. Centre-Ville, Montréal, QC H3C 3J7, Canada 5Institut für Kommunikationsnetze und Satellitenkommunikation, Inffeldgasse 12/I, 8010 Graz, Austria 6Department of Physics, Royal Military College of Canada, PO Box 17000, Stn Forces, Kingston, ON K7K 7B4, Canada 7Centrum Badan´ Kosmicznych, Polska Akademia Nauk, Bartycka 18A, 00-716 Warszawa, Poland 8Department of Astronomy and Astrophysics, University of Toronto, 50 St. George Street, Toronto, ON M5S 3H4, Canada 9Institut für Astro- und Teilchenphysik, Universität Innsbruck, Technikerstrasse 25/8, 6020, Innsbruck, Austria 10Department of Physics and Astronomy, University of British Columbia, Vancouver, BC V6T1Z1, Canada 11Silesian University of Technology, Institute of Automatic Control, Gliwice, Akademicka 16, Poland 12European Organisation for Astronomical Research in the Southern Hemisphere, Karl-Schwarzschild-Str. 2, 85748 Garching b. München, Germany 13LESIA, Observatoire de Paris, PSL Research University, CNRS, Sorbonne Universités, UPMC Univ. Paris 06, Univ. Paris Diderot, Sorbonne Paris Cité, 5 place Jules Janssen, F-92195 Meudon, France 14Institut de recherche sur les exoplanétes, iREx, Département de physique, Université de Montréal, Montréal, QC, H3C 3J7, Canada Abstract. -
Orbital Lifetime Predictions
Orbital LIFETIME PREDICTIONS An ASSESSMENT OF model-based BALLISTIC COEFfiCIENT ESTIMATIONS AND ADJUSTMENT FOR TEMPORAL DRAG co- EFfiCIENT VARIATIONS M.R. HaneVEER MSc Thesis Aerospace Engineering Orbital lifetime predictions An assessment of model-based ballistic coecient estimations and adjustment for temporal drag coecient variations by M.R. Haneveer to obtain the degree of Master of Science at the Delft University of Technology, to be defended publicly on Thursday June 1, 2017 at 14:00 PM. Student number: 4077334 Project duration: September 1, 2016 – June 1, 2017 Thesis committee: Dr. ir. E. N. Doornbos, TU Delft, supervisor Dr. ir. E. J. O. Schrama, TU Delft ir. K. J. Cowan MBA TU Delft An electronic version of this thesis is available at http://repository.tudelft.nl/. Summary Objects in Low Earth Orbit (LEO) experience low levels of drag due to the interaction with the outer layers of Earth’s atmosphere. The atmospheric drag reduces the velocity of the object, resulting in a gradual decrease in altitude. With each decayed kilometer the object enters denser portions of the atmosphere accelerating the orbit decay until eventually the object cannot sustain a stable orbit anymore and either crashes onto Earth’s surface or burns up in its atmosphere. The capability of predicting the time an object stays in orbit, whether that object is space junk or a satellite, allows for an estimate of its orbital lifetime - an estimate satellite op- erators work with to schedule science missions and commercial services, as well as use to prove compliance with international agreements stating no passively controlled object is to orbit in LEO longer than 25 years. -
Achievements of Hayabusa2: Unveiling the World of Asteroid by Interplanetary Round Trip Technology
Achievements of Hayabusa2: Unveiling the World of Asteroid by Interplanetary Round Trip Technology Yuichi Tsuda Project Manager, Hayabusa2 Japan Aerospace ExplorationAgency 58th COPUOS, April 23, 2021 Lunar and Planetary Science Missions of Japan 1980 1990 2000 2010 2020 Future Plan Moon 2007 Kaguya 1990 Hiten SLIM Lunar-A × Venus 2010 Akatsuki 2018 Mio 1998 Nozomi × Planets Mercury (Mars) 2010 IKAROS Venus MMX Phobos/Mars 1985 Suisei 2014 Hayabusa2 Small Bodies Asteroid Ryugu 2003 Hayabusa 1985 Sakigake Asteroid Itokawa Destiny+ Comet Halley Comet Pheton 2 Hayabusa2 Mission ✓ Sample return mission to a C-type asteroid “Ryugu” ✓ 5.2 billion km interplanetary journey. Launch Earth Gravity Assist Ryugu Arrival MINERVA-II-1 Deployment Dec.3, 2014 Sep.21, 2018 Dec.3, 2015 Jun.27, 2018 MASCOT Deployment Oct.3, 2018 Ryugu Departure Nov.13.2019 Kinetic Impact Earth Return Second Dec.6, 2020 Apr.5, 2019 Target Markers Orbiting Touchdown Sep.16, 2019 Jul,11, 2019 First Touchdown Feb.22, 2019 MINERVA-II-2 Orbiting MD [D VIp srvlxp #534<# Oct.2, 2019 Hayabusa2 Spacecraft Overview Deployable Xband Xband Camera (DCAM3) HGA LGA Xband Solar Array MGA Kaba nd Ion Engine HGA Panel RCS thrusters ×12 ONC‐T, ONC‐W1 Star Trackers Near Infrared DLR MASCOT Spectrometer (NIRS3) Lander Thermal Infrared +Z Imager (TIR) Reentry Capsule +X MINERVA‐II Small Carry‐on +Z LIDAR ONC‐W2 +Y Rovers Impactor (SCI) +X Sampler Horn Target +Y Markers ×5 Launch Mass: 609kg Ion Engine: Total ΔV=3.2km/s, Thrust=5-28mN (variable), Specific Impulse=2800- 3000sec. (4 thrusters, mounted on two-axis gimbal) Chemical RCS: Bi-prop. -
Highlights in Space 2010
International Astronautical Federation Committee on Space Research International Institute of Space Law 94 bis, Avenue de Suffren c/o CNES 94 bis, Avenue de Suffren UNITED NATIONS 75015 Paris, France 2 place Maurice Quentin 75015 Paris, France Tel: +33 1 45 67 42 60 Fax: +33 1 42 73 21 20 Tel. + 33 1 44 76 75 10 E-mail: : [email protected] E-mail: [email protected] Fax. + 33 1 44 76 74 37 URL: www.iislweb.com OFFICE FOR OUTER SPACE AFFAIRS URL: www.iafastro.com E-mail: [email protected] URL : http://cosparhq.cnes.fr Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law The United Nations Office for Outer Space Affairs is responsible for promoting international cooperation in the peaceful uses of outer space and assisting developing countries in using space science and technology. United Nations Office for Outer Space Affairs P. O. Box 500, 1400 Vienna, Austria Tel: (+43-1) 26060-4950 Fax: (+43-1) 26060-5830 E-mail: [email protected] URL: www.unoosa.org United Nations publication Printed in Austria USD 15 Sales No. E.11.I.3 ISBN 978-92-1-101236-1 ST/SPACE/57 *1180239* V.11-80239—January 2011—775 UNITED NATIONS OFFICE FOR OUTER SPACE AFFAIRS UNITED NATIONS OFFICE AT VIENNA Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law Progress in space science, technology and applications, international cooperation and space law UNITED NATIONS New York, 2011 UniTEd NationS PUblication Sales no. -
Attitude Control Dynamics of Spinning Solar Sail “IKAROS” Considering
Attitude Control Dynamics of Spinning Solar Sail “IKAROS” Considering Thruster Plume Osamu Mori, Yoji Shirasawa, Hirotaka Sawada, Ryu Funase, Yuichi Tsuda, Takanao Saiki and Takayuki Yamamoto (JAXA), Morizumi Motooka and Ryo Jifuku (Univ. of Tokyo) Abstract In this paper, the attitude dynamics of IKAROS, which is spinning solar sail, is presented. First Mode Model of out-of-plane deformation (FMM) and Multi Particle Model (MPM) are introduced to analyze the out-of-plane oscillation mode of spinning solar sail. The out-of-plane oscillation of IKAROS is governed by three modes derived from FMM. FMM is very simple and valid for the design of attitude controller. Considering the thruster configuration of IKAROS, the force on main body and sail by thruster plume as well as reaction force by thruster are integrated into MPM. The attitude motion after sail deployment or reorientation using thrusters can be analyzed by MPM numerical simulations precisely. スラスタプルームを考慮したスピン型ソーラーセイル「IKAROS」の姿勢制御運動 森 治,白澤 洋次,澤田 弘崇,船瀬 龍,津田 雄一,佐伯 孝尚,山本 高行(JAXA), 元岡 範純,地福 亮(東大) 摘要 本論文ではスピン型ソーラーセイル IKAROS の姿勢運動について示す.スピン型ソーラーセイル を解析するために一次面外変形モデルおよび多粒子モデルを導入する.まず,一次面外変形モデ ルから導出される 3 つのモードが IKAROS の面外運動を支配していることを示す.このモデルは 非常に簡易であり,姿勢制御設計に有効であると言える.一方,多粒子モデルに対しては, IKAROS のスラスタ配置を考慮して,スラスタの反力だけでなくスラスタプルームが本体や膜面 に及ぼす力を組み込み,セイル展開後およびスラスタによるマヌーバ後の姿勢運動を数値シミュ レーションにより詳細に解析する. 1. Introduction for the numerical model. Considering the thruster configuration of IKAROS, the force on main body and A solar sail 1) is a space yacht that gathers energy for sail by thruster plume as well as reaction force by propulsion from sunlight pressure by means of a thruster are integrated into MPM. The Fast Fourier membrane. The Japan Aerospace Exploration Agency Transform (FFT) results from IKAROS flight data are (JAXA) successfully achieved the world’s first solar sail compared with those from simulation data. -
Institutional Patterns in the Austrian Space Sector Wong, Annie; Van Burg, Elco; Giannopapa, Christina
VU Research Portal Institutional patterns in the Austrian space sector Wong, Annie; van Burg, Elco; Giannopapa, Christina published in Acta astronautica 2018 DOI (link to publisher) 10.1016/j.actaastro.2017.10.030 document version Publisher's PDF, also known as Version of record document license Article 25fa Dutch Copyright Act Link to publication in VU Research Portal citation for published version (APA) Wong, A., van Burg, E., & Giannopapa, C. (2018). Institutional patterns in the Austrian space sector. Acta astronautica, 142, 201-211. https://doi.org/10.1016/j.actaastro.2017.10.030 General rights Copyright and moral rights for the publications made accessible in the public portal are retained by the authors and/or other copyright owners and it is a condition of accessing publications that users recognise and abide by the legal requirements associated with these rights. • Users may download and print one copy of any publication from the public portal for the purpose of private study or research. • You may not further distribute the material or use it for any profit-making activity or commercial gain • You may freely distribute the URL identifying the publication in the public portal ? Take down policy If you believe that this document breaches copyright please contact us providing details, and we will remove access to the work immediately and investigate your claim. E-mail address: [email protected] Download date: 02. Oct. 2021 Acta Astronautica 142 (2018) 201–211 Contents lists available at ScienceDirect Acta Astronautica journal -
SGAC-Annual-Report-2014.Pdf
ANNUAL REPORT SPACE GENERATION ADVISORY COUNCIL 2014 In support of the United Nations Programme on Space Applications A. TABLE OF CONTENTS A. Table of Contents 2 In support of the United Nations Programme B. Sponsors and Partners 4 on Space Applications 1. Introduction 10 1.1 About the SGAC 12 14 c/o European Space Policy Institute (ESPI) 1.2 Letter from the Co-chairs 15 Schwarzenbergplatz 6 1.3 Letter from the Executive Director 16 Vienna A-1030 1.4 SGAC output at a glance AUSTRIA 2. SGAC Background 22 2.1 History of the SGAC 24 26 [email protected] 2.2 Leadership and Structure 27 www.spacegeneration.org 2.3 Programme +41 1 718 11 18 30 3. The organisation in 2014 30 32 +43 1 718 11 18 99 3.1 Goal Achievement Review 3.2 SGAC Activity Highlights 36 42 © 2015 Space Generation Advisory Council 3.3 Space Generation Fusion Forum Report 3.4 Space Generation Congress Report 50 3.5 United Nations Report 62 3.6 SGAC Regional Workshops 66 3.7 SGAC Supported Events 68 3.8 Financial Summary 72 Acknowledgements 4. Projects 78 4.1 Project Outcomes and Highlights 80 The SGAC 2014 Annual Report was compiled and 4.2 Space Technologies for Disaster Management Project Group 81 edited by Minoo Rathansabapathy (South Africa/ 4.3 Near Earth Objects Project Group 82 Australia), Andrea Jaime (Spain), Laura Rose (USA) 4.4 Space Law and Policy Project Group 84 and Arno Geens (Belgium) with the assistance of 4.5 Commercial Space Project Group 86 Candice Goodwin (South Africa), Justin Park (USA), 4.6 Space Safety and Sustainability Project Group 88 Nikita Marwaha (United Kingdom), Dario Schor 4.7 Small Satellites Project Group 90 (Argentina/Canada), Leo Teeney (UK) and Abhijeet 4.8 Space Exploration Project Group 92 Kumar (Australia) in editing. -
Space BD × Z-KAI Group × JAXA Started Educational Projects by Using "J-SPARC" Framework ~ Astronaut Training Method × Next Generation Type Education Project ~
Space BD × Z-KAI Group × JAXA Started Educational Projects by using "J-SPARC" Framework ~ Astronaut Training Method × Next Generation Type Education Project ~ November 13th 2018 Space BD Inc. Zoshinkai Holdings Inc. The Japan Aerospace Exploration Agency Space BD Inc. (CEO & Co-Founder Masatoshi Nagasaki, hereinafter "Space BD"), Zoshinkai Holdings Inc. (CEO Takaaki Fujii, hereinafter "Z-KAI Group") and The Japan Aerospace Exploration Agency (President Hiroshi Yamakawa, hereinafter "JAXA") started to create business in the education field in the framework of "J-SPARC" (JAXA Space Innovation through Partnership and Co-creation). By March 2019, Space BD will develop the Next Generation Type Education so-called "non- cognitive skills" method for all generations from children to adults (include corporate recruitment and training of companies) by analyze and evaluate the following items; (1) JAXA's Astronaut Training Method, (2) Experience and knowledge of Ms. Naoko Yamazaki (Astronaut), (3) Prof. Tatsuo Kitagawa’s Knowledge of international academic achievement evaluation tool / teaching material development record. Among the range of generation, Space BD collaborate with Z-KAI Group, which provides various educational services such as correspondence education and tutoring school, we will develop the programs (including teaching materials and program development) in the age group from children to university students. From April 2019, we will conduct test marketing and develop teaching materials for each age group. Finally, by April 2020, we aim for full- scale sales of the program and educational materials. JAXA will realize the maximization of JAXA research and development results not only in the space field, but also in the education field through provision of training methods for astronauts cultivated over many years. -
Mechanical & AEROSPACE Engineering Department
Mechanical & Aerospace Engineering Department 2012-13 UCLA MAE Chair’s Message Chair’s Message Dear Friends and Colleagues, I am pleased to present to you the Annual Report of the Mechanical and Aerospace Engineering Department. The Report presents highlights of the accomplishments and news of the Department’s alumni, students, faculty, and staff during the 2012-2013 Academic Year. As a member of the global higher education and research communities we strive to make significant contributions to these communities and to positively impact society. From reading these pages, I hope you will sense the pulse of our highly intellectual and vibrant community. Sincerely Yours, Tsu-Chin Tsao Tsu-Chin Tsao, Department Chair FRONT COVER: UCLA MAE NSF Center “Translational Applications of Nanoscale Multiferroic Systems (TANMS)” focuses on developing nanoscale memory, antenna, and motor elements, all essential components in miniature navigation systems. The cover figure shows an illustration of a miniature submarine the size of a red blood cell, reminiscent of the classic “Fantastic Voyage” movie of 1966. Here the TANMS elements are key barrier technologies to make this science fiction notion an actual device, important for medical and other applications. Image by Josh Hockel. Mission Statement Our mission is to educate the nation’s future leaders in the science and art of mechanical and aerospace engineering. Further, we seek to expand the frontiers of engineering science and to encourage technological innovation while fostering academic excellence -
Astronautilus-18.Pdf
Kosmos to dla nas najbardziej zaawansowana nauka, która często redefiniuje poglądy filozofów, najbardziej zaawansowana technika, która stała się częścią nasze- go życia codziennego i czyni je lepszym, najbardziej Dwumiesięcznik popularnonaukowy poświęcony tematyce wizjonerski biznes, który każdego roku przynosi setki astronautycznej. ISSN 1733-3350. Nr 18 (1/2012). miliardów dolarów zysku, największe wyzwanie ludz- Redaktor naczelny: dr Andrzej Kotarba kości, która by przetrwać, musi nauczyć się żyć po- Zastępca redaktora: Waldemar Zwierzchlejski Korekta: Renata Nowak-Kotarba za Ziemią. Misją magazynu AstroNautilus jest re- lacjonowanie osiągnięć współczesnego świata w każdej Kontakt: [email protected] z tych dziedzin, przy jednoczesnym budzeniu astronau- Zachęcamy do współpracy i nadsyłania tekstów, zastrze- tycznych pasji wśród pokoleń, które jutro za stan tego gając sobie prawo do skracania i redagowania nadesłanych świata będą odpowiadać. materiałów. Przedruk materiałów tylko za zgodą Redakcji. Spis treści PW-Sat: Made in Poland! ▸ 2 Polska ma długie tradycje badań kosmicznych – polskie instrumenty w ramach najbardziej prestiżowych misji badają otoczenie Ziemi i odległych planet. Ale nigdy dotąd nie trafił na orbitę satelita w całości zbudowany w polskich labo- ratoriach. Może się nim stać PW-Sat, stworzony przez studentów Politechniki Warszawskiej. Choć przedsięwzięcie ma głównie wymiar dydaktyczny, realizuje również ciekawy eksperyment: przyspieszoną deorbitację. CubeSat, czyli mały może więcej ▸ 15 Objętość decymetra sześciennego oraz masa nie większa niż jeden kilogram. Ta- kie ograniczenia konstrukcyjne narzuca satelitom standard CubeSat. Oryginalnie opracowany z myślą o misjach studenckich (bazuje na nim polski PW-Sat), Cu- beSat zyskuje coraz większe rzesze zwolenników w sektorze komercyjnym, woj- skowym i naukowym. Sprawdźmy, czym są i co potrafią satelity niewiele większe od kostki Rubika.